南安普顿大学的可持续能源研究小组在设计新型涡轮叶片和选址方面进展良好。
Work on designs for the new turbine blades and sites are well advanced at the University of Southampton's sustainable energy research group.
这蒸汽被用来推动发电机的涡轮叶片。
This steam is used to turn turbine blades of electric generators.
检查风扇叶片和涡轮叶片无损坏迹象。
这里的涡轮叶片部分之一。
涡轮叶片的造型是数控加工的前提条件。
The modeling of turbine blades is the premise for NC machining.
为涡轮叶片的冷却结构设计提供了依据。
涡轮叶片是航空发动机中的关键部件之一。
The turbine blade is one of the key components in aeroengine.
本文对涡轮叶片疲劳—蠕变试验技术进行了综合论述。
This paper has a general discussion on the technique of fatigue-creep experiment of turbine blade.
本文介绍了用解析法计算涡轮叶片喉道尺寸的方法和步骤。
The author provides a method and sequence for the analytical calculation of turbine blade throat path dimension.
开发了一个针对涡轮叶片模具活块的电极零件的CAD系统。
CAD system for three dimensional electrode of turbo blade mould part is developed in this paper.
实验中对涡轮叶片采用四排气膜孔的冷却方案，气膜孔为圆柱形。
The surface of a gas turbine blade was cooled by four rows of cylindrical holes in the experiment.
航空发动机空心涡轮叶片的壁厚是保证叶片强度的一个关键参数。
The wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength.
用计算几何的方法重构大型涡轮叶片曲面，可提高叶片的物理学性能；
Improvement of the physics performance of blade is obtained by reconstructing the large size surface of turbine blade based on calculation geometry.
本文的研究结果对准确评定镍基单晶涡轮叶片的剩余寿命具有参考作用。
The results of the paper can be used to precisely evaluate the remainder life of Nickel-based single crystal turbine blade.
涡轮叶片锯齿冠的设计对于保证发动机的可靠性、寿命和安全至关重要。
The structural design for serrated shroud of turbine blade was very important for the reliability, life and safety of aeroengine.
本文从实验和计算的角度对涡轮叶片中的流场、温度场耦合进行了研究。
The flow field and the temperature field in the turbine cascade were studied in view of experiment and computation.
研究了涡轮叶片材料M38G合金渗稀土-铝涂层的工艺过程和组织结构。
The RE-aluminizing technique and coating structure of gas turbine blade made of alloy M38G are studied.
涡轮叶片之间冷却空气缝隙的堵塞主要是因为存在高比表面积的超细粒子。
Clogging up of the cooling air slits in the turbine blades is primarily caused by ultrafine particles with a high specific surface area.
为确保电厂安全可靠地运转，必须对涡轮叶片和其他部件的老化受损情况进行定期检查。
The turbine blades and other components have to be inspected regularly for signs of aging in order to assure that the power plant works safely and reliably.
基于锥束体积CT的涡轮叶片质量检测技术是当前无损检测领域的研究热点。
Turbine blades quality inspection technology based on Cone Beam Volume ct has become hot point of current NDT research field.
着重介绍了气膜冷却、涡轮叶片内流冷却技术和气膜孔流量系数的研究进展。
Particular emphasis is given to the development of film cooling, internal cooling technologies and film hole discharge coefficients.
结果表明：增压器喷嘴环和涡轮叶片流通面积减少是涡轮增压器喘振的主要原因。
The results show that the reason why surge happened is that flow area of nozzle ring and blade was decreased.
本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。
In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically.
涡轮叶片内部冷却特性直接影响到叶片的壁面温度分布，必须对其展开详细的研究。
The temperature distribution of the nozzle guide vanes are affected greatly by the flow and heat transfer of the internal cooling passages.
研究结果对于定向凝固涡轮叶片设计、分析方法的完善和成形工艺的改进具有重要意义。
The research results may also help to improve the fabrication processes of directional turbine blade solidification.
飞机发动机涡轮叶片的内部结构相当复杂，这给叶片模具的分模设计带来了很大的困难。
The internal structure of turbo blade in plane engine is quite complex, which brings so much difficulty for parting design of turbo blade mould.
这种热应力与离心应力、气动应力合成的综合应力可能引起涡轮叶片的低循环疲劳失效。
The synthesis of thermal, centrifugal and aerodynamic stresses may cause the low cycle fatigue failure of the blades.
这种热应力与离心应力、气动应力合成的综合应力可能引起涡轮叶片的低循环疲劳失效。
The synthesis of thermal, centrifugal and aerodynamic stresses may cause the low cycle fatigue failure of the blades.
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